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    SMALL PROPULSION SYSTEMS

    FOR

    UN-MANNED AIR VEHICLES

    &

    MODEL AIRCRAFTCENGIZ CAMCI

    DEPARTMENT OF AEROSPACE ENGINEERING

    THE PENNSYLVANIA STATE UNIVERSITY

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    SMALL PROPULSION SYSTEMSFOR

    UNMANNED AND MODEL AIRCRAFT

    CONVENTIONALINTERNAL

    COMBUSTION

    RUBBERPOWERED

    ELECTRIC

    MOTOR

    POWERED

    GAS TURBINE /

    JET POWEREDSYSTEMS

    EXOTIC

    SYSTEMS

    TWO

    STROKE

    ENGINES

    FOURSTROK EENGINES

    CONVENTIONALFOUR CYCLE

    OTTOENGINE

    ROTARYENGINE

    Wankel engine

    ROTATINGCYLINDER VALVE

    ENGINE

    TURBO-JET SYST EMS

    FOR

    JET RPOPULSION

    TURBO-SHAFT SYSTEMS

    FOR PROPELLER

    AND

    ROTOR DRIVEN SYST EMS

    TURBO-SHAFTGAS

    TURBINE DRIVEN

    A SINGLE DC

    ELECTRIC

    GENERATOR

    &

    DISTRIBUTED

    ELECTRIC MOTORS

    CO2 ENGINES

    PULSE JET S

    MICRO-ROCKET

    LASER DRIVEN

    MIGRATINGCOMBUSTION

    CHAMBER

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    CONVENTIONAL INTERNAL

    COMBUSTION ENGINES

    TWO STROKE ENGINESMigrating Combustion Chamber Engine (MCC)

    FOUR CYCLE ENGINES

    Conventional Four Cycle (OTTO ENGINE)

    Rotary Engine (WANKEL)

    Rotating Cylinder Valve Engine (RCV)

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    TWO STROKE ENGINES +

    Two-stroke engines do not have valves,

    which simplifies their construction and

    lowers their weight.

    Two-stroke engines fire once every

    revolution, while four-stroke engines fire

    once every other revolution. This givestwo-stroke engines a significant power

    boost.

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    TWO STROKE ENGINES +

    These advantages make two-stroke engines lighter,

    simpler and less expensiveto manufacture.

    Two-stroke engines also have the potential to pack

    about twice the power into the same space

    because there are twice as many power strokes per

    revolution.

    The combination of light weight and twice the power

    gives two-stroke engines a great power-to-weight

    ratiocompared to many four-stroke engine designs.

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    TWO STROKE ENGINES +

    Two-stroke engines can work in any

    orientation, which can be important in

    inverted flights or acrobatic flights.

    A standard four-stroke engine may

    have problems with oil flow unless it

    is upright, and solving this problemcan add complexity to the engine.

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    TWO STROKE ENGINES -

    Two-stroke engines don't last nearly as

    long as four-stroke engines. The lack of

    a dedicated lubrication system means

    that the parts of a two-stroke engine

    wear a lot faster.

    Two-stroke oil is expensive, and you

    need about 4 ounces of it per gallon ofgas. You would burn about a gallon of

    oil every 1,000 miles if you used a two-

    stroke engine in a car.

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    TWO STROKE ENGINES -

    Two-stroke engines do not use fuel

    efficiently, so you would get fewer miles

    per gallon.

    Two-stroke engines produce a lot of

    pollution

    -- so much, in fact, that it is likely that you

    won't see them around too much longer.

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    FUEL

    INTAKE

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    COMPRESSION

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    COMBUSTION

    &

    EXHAUST

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    TWO STROKE

    OPERATION

    TWO STROKE

    OPERATION

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    USEFUL ENGINE SIZING

    CORRELATION(only for two stroke engines)

    1 cubic inch of displacement

    will handle

    10 lbs of aircraft weight

    1 cubic inch is 16 cc

    1 HP = 0.735 KW

    1KW = 1.359 HP (metric)

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    SMALL PROPULSION SYSTEMSFOR

    UNMANNED AND MODEL AIRCRAFT

    CONVENTIONAL

    INTERNAL

    COMBUSTION

    RUBBERPOWERED

    ELECTRIC

    MOTORPOWERED

    GAS TURBINE /

    JET POWEREDSYSTEMS

    EXOTIC

    SYSTEMS

    TWO

    STROKE

    ENGINES

    FOUR

    STROK EENGINES

    CONVENTIONAL

    FOUR CYCLEOTTO

    ENGINE

    ROTARYENGINE

    Wankel engine

    ROTATINGCYLINDER VALVE

    ENGINE

    TURBO-JET SYST EMS

    FOR

    JET RPOPULSION

    TURBO-SHAFT SYSTEMS

    FOR PROPELLER

    AND

    ROTOR DRIVEN SYST EMS

    TURBO-SHAFTGAS

    TURBINE DRIVEN

    A SINGLE DC

    ELECTRIC

    GENERATOR

    &

    DISTRIBUTED

    ELECTRIC MOTORS

    CO2 ENGINES

    PULSE JET S

    MICRO-ROCKET

    LASER DRIVEN

    MIGRATINGCOMBUSTION

    CHAMBER

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    DUAL MIGRATING

    COMBUSTION

    CHAMBERS

    TWO STROKE CYCLE

    19.7 cm3 (1.2 cu.in)

    2.2 HP @ 7000 rpm

    Compression = 7.39

    Weight = 38.7 oz.

    1 oz./min

    MIGRATING COMBUSTION CHAMBERERICKSON ENGINE

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    Instant starting ability

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    SMALL PROPULSION SYSTEMSFOR

    UNMANNED AND MODEL AIRCRAFT

    CONVENTIONAL

    INTERNAL

    COMBUSTION

    RUBBERPOWERED

    ELECTRIC

    MOTORPOWERED

    GAS TURBINE /

    JET POWEREDSYSTEMS

    EXOTIC

    SYSTEMS

    TWO

    STROKE

    ENGINES

    FOUR

    STROK EENGINES

    CONVENTIONAL

    FOUR CYCLEOTTO

    ENGINE

    ROTARYENGINE

    Wankel engine

    ROTATINGCYLINDER VALVE

    ENGINE

    TURBO-JET SYST EMS

    FOR

    JET RPOPULSION

    TURBO-SHAFT SYSTEMS

    FOR PROPELLER

    AND

    ROTOR DRIVEN SYST EMS

    TURBO-SHAFTGAS

    TURBINE DRIVEN

    A SINGLE DC

    ELECTRIC

    GENERATOR

    &

    DISTRIBUTED

    ELECTRIC MOTORS

    CO2 ENGINES

    PULSE JET S

    MICRO-ROCKET

    LASER DRIVEN

    MIGRATINGCOMBUSTION

    CHAMBER

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    FOUR CYCLE ENGINES

    conventional Otto engines

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    FOUR CYCLE ENGINE OPERATION

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    FOUR CYCLE ENGINE

    CHARACTERISTICS

    FOUR STROKE ENGINES LASTS LONGER THAN TWO STROKE ENGINES. The

    lack of a dedicated lubrication system means that the parts of a two-stroke engine

    wear a lot faster.

    FOUR STROKE ENGINES DONT BURN OIL IN COMBUSTION CHAMBER. Two-

    stroke oil is expensive, and you need about 4 ounces of it per gallon of gas. You

    would burn about a gallon of oil every 1,000 miles if you used a two-stroke engine in

    a car.

    FOUR STROKE ENGINES ARE MORE FUEL EFFICIENT. Two-stroke engines do

    not use fuel efficiently, so you would get fewer miles per gallon.

    FOUR STROKE ENGINES ARE CLEANER. Two-stroke engines produce a lot ofpollution

    INVERTED FLIGHTS MAY NOT BE EASY IN FOUR STROKE ENGINES.Two-

    stroke engines can work in any orientation, which can be important in acrobatic

    flights. A standard four-stroke engine may have problems with oil flow unless it is

    upright, and solving this problem can add complexity to the engine.

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    Unusual

    Four stroke engines forUAV/MAV applications

    ROTARY CYLINDER VALVE ENGINE RCV ENGINE

    ROTARY ENGINES WANKEL ENGINE

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    ROTARY ENGINES

    Wankel Engine

    Rotary engines use the four-stroke combustion

    cycle, which is the same cycle that four-stroke

    piston engines use. But in a rotary engine, this is

    accomplished in a completely different way.

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    The heart of a rotary engine is the rotor.This is roughly the

    equivalent of the pistons in a piston engine. The rotor is

    mounted on a large circular lobe on the output shaft. This

    lobe is offset from the centerline of the shaft and acts like the

    crank handle on a winch, giving the rotor the leverage it

    needs to turn the output shaft. As the rotor orbits inside the

    housing, it pushes the lobe around in tight circles, turning

    three timesfor every one revolution of the rotor.

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    How Rotary Engines Work

    For everythree rotations

    of the engineshaftcorresponds toone complete

    piston rotation

    (360 degrees)

    WANKEL ENGINE OPERATION

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    How Rotary Engines Work

    If you watch carefully, you'll see the offset

    lobe on the output shaft spinning three times

    for every complete revolution of the rotor.

    As the rotor moves through the

    housing, the three chambers

    created by the rotor change size.

    This size change produces apumping action. Let's go through

    each of the four stokes of the

    engine looking at one face of the

    rotor.

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    A subminiature rotary engine

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    A subminiature rotary engine

    for unmanned aircraft

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    ROTATING CYLINDER VALVE

    ENGINE

    SINGLE CYLINDER

    4-STROKE CYCLE

    20.02 cm3(1.2 cu.in.)weight = 37.1 oz.

    Compression = 10.5

    1.8 HP @ 5,800rpm

    .85 oz/min

    mailto:HP@5,800mailto:HP@5,800
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    ROTARY CYLINDER VALVE ENGINE

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    SMALL PROPULSION SYSTEMSFOR

    UNMANNED AND MODEL AIRCRAFT

    CONVENTIONAL

    INTERNALCOMBUSTION

    RUBBER

    POWERED

    ELECTRIC

    MOTORPOWERED

    GAS TURBINE /

    JET POWEREDSYSTEMS

    EXOTIC

    SYSTEMS

    TWO

    STROKE

    ENGINES

    FOUR

    STROK EENGINES

    CONVENTIONAL

    FOUR CYCLEOTTOENGINE

    ROTARYENGINE

    Wankel engine

    ROTATINGCYLINDER VALVE

    ENGINE

    TURBO-JET SYST EMS

    FOR

    JET RPOPULSION

    TURBO-SHAFT SYSTEMS

    FOR PROPELLER

    AND

    ROTOR DRIVEN SYST EMS

    TURBO-SHAFTGAS

    TURBINE DRIVEN

    A SINGLE DC

    ELECTRIC

    GENERATOR

    &

    DISTRIBUTED

    ELECTRIC MOTORS

    CO2 ENGINES

    PULSE JET S

    MICRO-ROCKET

    LASER DRIVEN

    MIGRATINGCOMBUSTION

    CHAMBER

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    OTHER

    SYSTEMS

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    are needed to s ee this picture .

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    NASA-CW LASER POWERED MODEL AIRCRAFT

    SOLAR

    CELLS

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    SEIKO-EPSON FLYING CAMERA

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    1. C. Hall "Skip" Jones, "Converting

    Auto Engines For Aircraft

    Applications," Sport Aviation, April1993.

    2. Edward F. Obert,Internal

    Combustion Engines, 3rd ed.

    (Scranton, PA: International Textbook

    Company, 1968).